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Drag-free control for cold air thrusters based on variable universe adaptive fuzzy PID

机译:基于可变宇宙自适应模糊PID的冷空推进器无阻力控制

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Cold air micro-thruster is a multi-variable, nonlinear, strong coupling system. The traditional control method is vulnerable to uncertain factors such as the satellite parameters change and load disturbance. It is difficult to obtain satisfactory control effect. This paper puts forward an adaptive variable universe fuzzy PID compound control strategy, control parameters is realized by using fuzzy control and variable region since the setting and control rules of self-adjustment. Apply it to the drag-free control of cold air thrusters based on the micro-thrust loop, the results show that the method has fast dynamic response, strong anti-interference ability and robustness, etc.
机译:冷空气微推进器是一种多变量,非线性强的耦合系统。 传统的控制方法容易受到诸如卫星参数变化和负载干扰等不确定因素的因素。 很难获得令人满意的控制效果。 本文提出了一种自适应变量宇宙模糊PID化合物控制策略,通过自动调整的设置和控制规则,通过使用模糊控制和可变区域来实现控制参数。 将其应用于基于微推力环的冷空炮推进器的无阻力控制,结果表明该方法具有快速的动态响应,强烈的抗干扰能力和鲁棒性等。

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